1 fatality

2010-03-04: Cessna 303 Crusader (N9305T) — James A. Youngquist — Louisa, United States of America

Louisa, United States of AmericaTakeoff (climb)

On March 4, 2010, a Cessna 303 Crusader (registration N9305T) operated by James A. Youngquist was involved in an aviation accident near Louisa, United States of America during takeoff. One person was killed. Investigators recorded the probable cause as: The pilot's failure to maintain aircraft control and secure the right engine during a loss of engine power after takeoff. Contributing to the accident was the loss of engine power on the right engine for undetermined reasons. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781196230Data APIEditorial standards

During takeoff, witnesses observed rough engine operation and smoke before the airplane rolled left and descended into a residence. Maintenance records show prior right engine work and a fuel flow reset contrary to procedures. Examination revealed no preimpact mechanical malfunctions but propeller signatures indicated power asymmetry.

Accident Sequence

During takeoff, one witness noted that at least one engine seemed to be running rough and not making power. Several other witnesses, located about half a mile northwest of the airport, observed the accident airplane pass overhead in a right turn. They reported that the engine noise did not sound normal. Two of the witnesses noted grayish black smoke emanating from the airplane. The airplane then rolled left and descended nose down into the front yard of a residence.

Maintenance History

Review of maintenance records revealed that the airplane underwent an annual inspection and extensive maintenance about three months prior to the accident. One of the maintenance issues was to troubleshoot the right engine that was reportedly running rough at cruise. During the maintenance, the right engine fuel pump, metering valve, and fuel manifold were removed and replaced with overhauled units. Additionally, the right engine fuel flow was reset contrary to procedures contained in an engine manufacturer service information directive. However, the fuel pump could not be tested due to thermal damage, and the investigation could not determine if the fuel flow setting procedure contributed to the loss of power on the right engine.

Examination Findings

On-scene examination of the wreckage and teardown examination of both engines did not reveal any preimpact mechanical malfunctions. Teardown examination of the right propeller revealed that the blades were not at or near the feather position, which was contrary to the emergency procedure published by the manufacturer to secure the engine and feather the propeller in the event of an engine power loss. The right propeller exhibited signatures consistent with low or no power at impact, while the left propeller exhibited signatures consistent with being operated with power at impact.

Probable Cause

The official probable cause, as stated by the investigation, is: The pilot's failure to maintain aircraft control and secure the right engine during a loss of engine power after takeoff. Contributing to the accident was the loss of engine power on the right engine for undetermined reasons.